Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '172K' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '172K' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR EY2R9600695Retain Bearing · corrodedRETAIN BEARING FOUND CORRODED.SDR EY2R9600694Retain Bearing · corrodedRETAIN BEARING FOUND CORRODED.SDR EY2R9600693Retain Bearing · corrodedRETAIN BEARING FOUND CORRODED.SDR EY2R9600558Bearing Race · corrodedBEARING RACE CORRODED.SDR 96ZZZX2185Valve · crimp nut looseLYCOMING SB 518C APPLIES, NUT LOOSE ON END OF VERNATHERM, PROBABLY DUE TO VIBRATION. REPLACED DEFECTIVE PART WITH A NEW PART NOT CALLED OUT IN THE SERVICE BULLETIN.SDR 96ZZZX2042Fitting · crackedDURING 100-HOUR INSPECTION, THE RT INBOARD MAIN GEAR LEG SUPPORT FITTING WAS FOUND CRACKED AT U-BOLT ATTACH HOLE. REMOVAL OF GEAR LEG REVEALED THE CRACK STARTED UNDER THE NUT. SUSPECT CAUSE IS HIGH TIME/FATIGUE. SUBMITTER STATED CLOSE ATTENTION TO THIS AREASDR 96ZZZX2040U-Bolt · brokenDURING 100-HOUR INSPECTION, FOUND MAIN GEAR ATTACHMENT U-BOLT BROKEN ON ONE END. UPON REMOVAL OF THE MAIN GEAR LEG, THE REMAINING AN6-15A BOLT ATTACHING THE GEAR WAS FOUND BENT. SUBMITTER STATED HIGH/TIME FATIGUE IS SUSPECT CAUSE AND A TIME LIMIT ON THIS PARSDR 96ZZZX2054Casting · sheared rivetsA 1971 MODEL AND 1980 MODEL 172, FOUND WITH RIVETS SHEARED AND LOOSE WHICH ATTACH NOSE GEAR BUTTERFLY CASTING; THUS, CAUSING CASTING TO WORK AGAINST FIREWALL. THE TOP TWO BOLTS AT TOP WERE ONLY ATTACHING POINTS LEFT. CESSNA SM ALLOWS RIVET HOLES TO BE DRILLESDR 96ZZZX3566Impulse Coupler · excess wearDURING ROUTINE MAINTENANCE (COMPRESSION CHECK) ENGINE 'LOCKED UP.' UPON INVESTIGATION/EXAMINATION, IMPULSE COUPLER PAWL AND PAWL AXIS FOUND EXTREMELY WORN ALLOWING IMPULSE COUPLING TO JAM INTERMITTENTLY WITH NO WARNING.SDR 96ZZZX943Control Cable · brokenTRIM CABLE FOUND RUSTED AND PULLEY 'FROZEN'. THE CABLE BROKE WHEN THE TRIM WAS ACTUATED.SDR 96ZZZX942Track · corrodedINTERGRANULAR CORROSION FOUND 8 INCHES AFT OF LEADING EDGE ON SEAT TRACK, RT PASSENGER SIDE.SDR EY2R9600306Split Retainer · corrodedSPLIT RETAINER FOUND TO BE CORRODED.SDR EY2R9600305Bearing Race · corrodedBEARING RACE FOUND WITH CORROSION.SDR 96ZZZX48Venturi · defectiveC/W AD 93-18-03 BY REMOVING TWO-PIECE VENTURI AND INSTALLING CONSOLIDATED FUEL SYSTEM'S ONE-PIECE VENTURI. THEREAFTER, PILOT REPORTED CRUISE FLIGHT FUEL BURN INCREASED FROM 7 GPH TO 9 GPH. INSPECTION OF CARBURETOR AND VENTURI DISCLOSED NO DISCREPANCIES, BUT
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